FR1258

Looking at the Restart states from Rev 1259 we have the following results for FR1258
FR1258		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	PC error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)			
MMS1	Oct 21 2021 21:39:16	97670.601	97655.614	97655.650	-14.987	-14.951	-0.037	0.244%	0.121%	
MMS2	Oct 21 2021 21:39:35	97670.902	97656.049	97656.094	-14.853	-14.808	-0.045	0.301%	-3.369%	
MMS3	Oct 21 2021 21:40:36	97670.699	97670.699	97670.737	0.000	0.038	-0.038			
MMS4	Oct 21 2021 21:41:05	97670.947	97684.990	97685.080	14.042	14.133	-0.091	-0.645%	0.296%	
 
Note that MMS2 plane change was an order of magnitude small than that of MMS1.
MMS1 was 0.3134 m/s (net delta-v) and 16.71% axial, MMS2 was 0.2393 m/s and 28.24% axial, and MMS4 was 0.3969 m/s and 60.78% axial.
The Table below provides the following information:
•	The start and end times and planned maneuver 
•	Total delta-V (DeltaV_X, DeltaV_Y, and DeltaV_Z) for the first maneuver extracted from the DVTABLE files, 
•	The associated predicted velocity maneuver planning requirement for 1 and 2 orbit predictions (DeltaV_X Req, DeltaV_Y Req, and DeltaV_Z Req)
•	The difference between the predicted velocity and the GEONS definitive velocity at the start time of the first maneuver (Diff_V_X, Diff_V_Y, and Diff_V_Z).Planned maneuver total delta-V values based on the associated DVTABLEs    
As shown in the table below, all meet the requirement.

Maneuver ID	Timespan	DVX (m/s)/ 
Req. (m/s)/
DiffVX(m/s)	DVY (m/s)/
Req. (m/s)/
DiffVY(m/s)	DVZ (m/s)/
Req. (m/s)/
DiffVZ(m/s)	
MMS4_FR1258	2021_292/11:26:12 to 2021_292/11:27:22		-0.1259	0.0357	0.3712	
		0.01	0.01	0.01	
		0.0005497	0.003956	-0.001504	
MMS2_FR1258	2021_292/13:01:12 to 2021_292/13:01:32		0.0773	-0.2281	-0.0075	
		0.01	0.01	0.01	
		0.002825	0.0001845	-0.001939	
MMS1_FR1258	2021_292/14:36:12 to 2021_292/14:36:42		0.3021	0.0737	-0.0111	
		0.01	0.01	0.01	
		0.004438	0.000937	-0.001429